In general, this methodology allows working with any number of regions. This computational model consists of three parts (regions). We consider following regions:
rotor is rotational part of the model, fluid is flowing over rotating turbine wheel
2 statorsare static parts of the model, fluid is flowing through
spiral
drafttube
[spiral (stator)]
[drafttube (stator)]
Figure: Three regions of computational model: spiral; rotor; drafttube;
During simulation, each region is computed individually and each region communicates with other regions through special boundary conditions.